DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) 13.A Small Business Technology Transfer (STTR) Program Proposal Submission Instructions

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DARPA
-

1


DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA)

13.A

Small Business
Technology Transfer

(
STTR
)

Program

Proposal Submission Instructions



1.1 Introduction:


DARPA’s mission is to prevent technological surprise for the United States and to create technolo
gical
surprise for its adversaries. The DARPA SBIR and STTR Programs are designed to provide small, high
-
tech businesses and academic institutions the opportunity to propose radical, innovative, high
-
risk
approaches to address existing and emerging nation
al security threats; thereby supporting DARPA’s
overall strategy to bridge the gap between fundamental discoveries and the provision of new military
capabilities.


The responsibility for implementing DARPA’s Small Business
Technology Transfer

(
STTR
) Progra
m
rests with the Small Business Programs Office.


DEFENSE ADVANCED RESEARCH PROJECTS AGENCY

Attention: DIRO/SBPO

675

North
Randolph

Street

Arlington, VA 22203
-
2
114

(703) 526
-
4170

Home Page
http://www.darpa.mil/Opportunities/SBIR_STTR/SBIR_STTR.aspx


Offerors responding to the DARPA topics must follow all the instructions provided in the DoD Program
Solicitation. Specific DARPA requirements in addition to or that deviate from the D
oD Program
Solicitation are provided below and reference the appropriate section of the DoD Solicitation.


SPECIFIC DARPA REQUIREMENTS

The solicitation has been EXTENSIVELY rewritten and follows the changes of the
STTR

reauthorization. Please read the enti
re DoD solicitation and DARPA instructions carefully prior to
submitting your proposal. Please go to

http://content.govdelivery.com/bulletins/gd/USSBA
-
4cada5#

to
read the
STTR

Policy
Directive issued by the
Small Business Administration.


3.0 DEFINITIONS


3.
4

Export Control

The following will apply to all projects with military or dual
-
use applications that develop beyond
fundamental research (basic and applied research ordinarily publ
ished and shared broadly wi
thin the
scientific community):


(1) The Contractor shall comply with all U. S. export control laws and regulations, including the
International Traffic in Arms Regulations (ITAR), 22 CFR Parts 120 through 130, and the Export
Adm
inistration Regulations (EAR), 15 CFR Parts 730 through 799, in the performance of this contract.
In the absence of available license exemptions/exceptions, the Contractor shall be responsible for
obtaining the appropriate licenses or other approvals, if
required, for exports of (including deemed
exports) hardware, technical data, and software, or for the provision of technical assistance.


(2) The Contractor shall be responsible for obtaining export licenses, if required, before utilizing foreign
persons
in the performance of this contract, including instances where the work is to be performed on
-
site
DARPA
-

2


at any Government installation (whether in or outside the United States), where the foreign person will
have access to export
-
controlled technologies, includ
ing technical data or software.


(3) The Contractor shall be responsible for all regulatory record keeping requirements associated with the
use of licenses and license exemptions/exceptions.


(4) The Contractor shall be responsible for ensuring that the pr
ovisions of this clause apply to its
subcontractors.


Please visit
http://www.pmddtc.state.gov/regulations_laws/itar.html

for more detailed information
regarding ITAR requirements.


3.
5

Foreign National

ALL offerors proposing to use foreign nationals MUST follow Section
5.
4.c.
(8) of the DoD Program
Solicitation and disclose this information regardless of whether the topic i
s subject to ITAR restrictions.


4.0 PROPOSAL FUNDAME
NTALS


4.6
Cl
assified Proposals

DARPA topics are unclassified; however, the subject matter may be considered to be a “critical technology”
and therefore subject to ITAR restrictions. See
Export Control
requirements below in Section
3.3.


4.10 Debriefing

DARPA will pro
vide
a
debriefing to
the
offeror in accordance with FAR Subpart 15.5. The notification
letter will provide instructions for requesting a proposal debriefing. Small Businesses will receive a
notification for each proposal submitted. Please read each notif
ication carefully and note the proposal
number and topic number referenced. All communication from the DARPA will originate from the
sbir@darpa.mil

e
-
mail address. Please white
-
list this address in your company’s sp
am filters to ensure
timely receipt of communications from our office.


Notification of Proposal Receipt

After the solicitation closing date,
the person listed as the “Corporate Official” on the
Proposal
Coversheet will
receive
an e
-
mail with instructions
for retrieving
a proposal
acknowledg
ement
receipt
from the DARPA SBIR/STTR Information Portal.


Information on Proposal Status

Once the source selection is complete,
the person listed as the
“Corporate Official” on the Proposal
Coversheet
will receive an e
mail
with instructions for retrieving
a
letter of selection or non
-
selection from
the DARPA SBIR/STTR Information Portal.


5.0

PHASE I PROPOSAL


A Phase I Cost Volume ($1
0
0,000 maximum) must be submitted in detail online via the DoD
SBIR/STTR submission sy
stem.

Offerors are REQUIRED to use the online
C
ost
Volume

for the Phase I
and Phase I Option costs (available on the D
oD SBIR/STTR submission site).


Technical Assistance

In accordance with the
Small Business Act (15 U.S.C. 632)
, DARPA will authorize
the
recipient of a

Phase I STT
R award to purchase

technical assistance services, such as access to a network of scientists
and engineers engaged in a wide range of technologies, or access to technical and business literature
available through on
-
line data base
s, for the purpose of assisting such concerns in


DARPA
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3


A.

making better technical decisions concerning such projects;

B.

solving technical problems which arise during the conduct of such projects;

C.

minimizing technical risks associated with such projects; and

D.

developi
ng and commercializing new commercial products and processes resulting from such
projects.


If you are interested in proposing use of a vendor for technical assistance, you must provide a cos
t
breakdown

under “Other Direct Costs (ODCs)”
of the Cost Volume
and provide a one page description of
the vendor you will use and the technical assistance you will receive. The proposed
amount
may not
exceed $5,000 and the description sho
uld be included as the LAST page of the Technical Volume. This
description
will n
ot count against the 20
-
page limit and will NOT be evaluated
. Approval of technical
assistance is
not

guaranteed

and is subject to review of the contracting officer.


Human or Animal
Subject Research

DARPA discourages offerors from proposing to conduct
Human or Animal Subject Research during
Phase 1 due to the significant lead time required to prepare the documentation and obtain approval, which
will delay the Phase 1 award.


5.3 (c) (6)
Commercialization Strategy

DARPA is
equally
interested in
dual use
commercialization

of
STT
R project results to the U.S. military
,

the private sector market
,
or both,
and expects explicit discussion of
key activities to achieve this result
in
the commercialization strategy part of the proposal. Th
e

discussion

should inclu
de identification of the
problem, need, or requirement
relevant to a Department of Defense application and/or a
private sector
application
that the
STTR

project results would address; a description of how wide
-
spread and significant
the problem, need, or r
equirement is;
and
identification of the potential
DoD
end
-
users
, Federal
customers, and/or
private sector
customers

who w
ould likely use the technology.


Technology commercialization and transition from Research and Development activities to fielded
syste
ms within the DoD is challenging. Phase I is the time to plan for and begin transition
and
commercialization
activities. The small business must convey an understanding of the
preliminary
transition path or paths to be established during the Phase I proje
ct. That plan should include the
Technology Readiness Level (TRL)
expected
at the end of the Phase I. The plan should include
anticipated business model and
potential
private sector
and federal partners the company has identified to
support transition
an
d commercialization
activities.
In addition,
key proposed milestones anticipated
during Phase II
such as
: prototype development, laboratory and systems testing, integration, testing in
operational environment, and demonstrations.


5.5
Phase I Proposal Che
cklist:


The following criteria must be met or your proposal may be REJECTED.


____1. Include a header with company name, proposal number and topic number to each page of your
technical volume.

____2
. Break out subcontractor, material and travel costs i
n detail. Use the "Explanatory Material Field"
in the DoD
C
ost
Volume

worksheet for this information, if necessary.

____3
. The base effort does not exceed $100,000.

____4
. The technical volume does not exceed twenty (20) pages. Any page beyond 20 will
be redacted
prior to evaluations.

____
5
. Upload the Volume 1: Proposal Cover Sheet; Volume 2: Technical Volume; Volume 3: Cost
Volume; and Volume 4: Co
mpany Commercialization Report
electronically through the DoD submission
site by
6:00

am ET,
27 March
2013
.

DARPA
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4


____
6
. After uploading your file on the DoD submission site, review it to ensure that
all pages have
transferred
correctly

and do not contain unreadable characters
. Contact the DoD Help Desk immediately
with any problems.


6.0 PHASE I EVALUATION C
RITERIA


The offeror's attention is directed to the fact that non
-
Government advisors to the Government may
review and provide support in proposal evaluations during source selection. Non
-
government advisors
may have access to the offeror's proposals, may

be utilized to review proposals, and may provide
comments and recommendations to the Government's decision makers. These advisors will not establish
final assessments of risk and will not rate or rank offeror's proposals. They are also expressly prohibi
ted
from competing for DARPA SBIR or STTR awards in the SBIR/STTR topics they review and/or provide
comments on to the Government. All advisors are required to comply with procurement integrity laws
and are required to sign Non
-
Disclosure and Rules of Con
duct/Conflict of Interest statements. Non
-
Government technical consultants/experts will not have access to proposals that are labeled by their
proposers as "Government Only."


Please note that qualified advocacy letters will count towards the proposal pag
e limit and will be
evaluated towards criterion C.


Advocacy letters are not required for Phase I.


Consistent with Section 3
-
209 of DoD 5500.7
-
R, Joint Ethics Regulation, which as a general rule prohibits endorsement and
preferential treatment of a non
-
fe
deral entity, product, service or enterprise by DoD or DoD employees in
their official capacities,
letters from government personnel will NOT be considered during the evaluation
process
.


A qualified advocacy letter is from a relevant commercial procuring
organization(s) working with a DoD
or other Federal entity, articulating their pull for the technology (i.e., what need the technology supports
and why it is important to fund it), and possible commitment to provide additional funding and/or insert
the tec
hnology in their acquisition/sustainment program. If submitted, the letter should be included as the
last page of your technical upload.


Advocacy letters which are faxed or e
-
mailed separately will NOT be
considered.


Limitations on Funding

DARPA reserves

the right to select and fund only those proposals considered to be of superior quality and
highly relevant to the DARPA mission. As a result, DARPA may fund
multiple
proposal
s

in a topic area
,

or it may not fund
any proposals in a topic area.


7.0 PHASE
II PROPOSAL


Firms will receive a notification letter after 150 days (from the contract start date) with instructions for
preparing and submitting a
Phase II Proposal
and a deadline for submission
.

Visit
http://www.darpa.mil/Opportunities/SBIR_STTR/SBIR_Program.aspx

for more information regarding
the Phase II proposal process.


10
.0 CONTRACTUAL CONSI
DERATIONS


Type of Funding Agreement (Phase I)



DARPA Phase I awards will be Firm

Fixed Price contracts.



Companies that choose to collaborate with a University must highlight the research that is
being performed by the University and verify that the work is FUNDAMENTAL
RESEARCH.

DARPA
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Companies are strongly encouraged to pursue implementing
a government acceptable cost
accounting system during the Phase I project to avoid delay in receiving a Phase II award.
Visit
www.dcaa.mil

and download the “Information for Contractors” guide for more
information.


Average

Dollar Value of Awards (Phase I)

DARPA Phase I
awards
shall not exceed $100,000

for the base effort and shall not exceed $50,000 for
the option if exercised
.


Publication Approval (
Public Release)

NSDD 189 established the national policy for controlling t
he flow of scientific, technical, and engineering
information produced in federally funded fundamental research at colleges, universities, and laboratories.
The directive defines fundamental research as follows: ''Fundamental research' means basic and appl
ied
research in science and engineering, the results of which ordinarily are published and shared broadly
within the scientific community, as distinguished from proprietary research and from industrial
development, design, production, and product utilizati
on, the results of which ordinarily are restricted for
proprietary

or national security reasons."


It is DARPA’s goal to eliminate pre
-
publication review and other restrictions on fundamental research
except in those exceptional cases when it is in the bes
t interest of national security. Please visit
http://www.darpa.mil/NewsEvents/Public_Release_Center/Public_Release_Center.aspx

for additional
information and a
pplicable publication approval procedures. Visit
http://dtsn.darpa.mil/fundamentalresearch/

to verify whether or not your award has a pre
-
publication
review requirement.


10
.7

Phase I Report
s

All DA
RPA Phase I awardees are required to submit
reports in accordance with the
C
ontract Data
Requirements List


CDRL and any applicable
Contract Line Item Number

(CLIN) of the Phase I
contract.

R
eport
s

must be provided to the individuals identified in Exhibi
t A of the contract.


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DARPA STTR 13.A Topic Index



ST13A
-
001


Functional Imaging to Develop Outstanding Service
-
Dogs (FIDOS)

ST13A
-
002


High
-
bandwidth, Low
-
sensitivity Optomechanical MEMS Accelerometers

ST13A
-
003


Development of Gravitational Radiatio
n Technology for Military Applications

ST13A
-
004


A Flexible and Extensible Solution to Incorporating New RF Devices and Capabilities

into EW/ ISR Networks

ST13A
-
005


Modeling and Optimizing Turbines for Unsteady Flow

ST13A
-
006


Novel Extensible Design App
roaches for Advanced Aircraft Composite Structural

Architectures

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7


DARPA STTR 13.A Topic Descriptions



ST13A
-
001


TITLE:
Functional Imaging to Develop Outstanding Service
-
Dogs (FIDOS)


TECHNOLOGY AREAS: Human Systems


OBJECTIVE: This effort will capitalize

on first
-
of
-
its
-
kind neural imaging feasibility work; demonstrating
functional brain activation in unrestrained dogs in response to handler cues. The objective of this effort is two
-
fold;
first, to optimize the selection of ideal service dogs, both in ope
rational military and therapy environments, and
second, to use real
-
time neural feedback to optimize canine training, shortening training duration, reducing costs,
and increasing learned responses.


DESCRIPTION: Military working dogs are used in a variety

of operations, including bomb detection, search and
rescue, and drug interdiction. Service dogs are also utilized in clinical settings, as therapy dogs to mitigate
symptoms of Post
-
Traumatic Stress Disorder (PTSD) and Traumatic Brain Injury (TBI) in retur
ning service
members. Certain dog breeds, ideal for this work, are rare (a limiting resource) and variability in dog training and
performance limits their effectiveness in operational environments. Better selection and screening of service dogs
would ensur
e that the best dogs, with optimal motivation and trainability are selected for service. Current training
regimens are driven by classic behaviorism, involving simple reward/punishment conditioning. They are time
-
intensive and costly, costing more than $20
,000 per dog
-
human pair (in clinical animal
-
human work pairs).
Therefore, this program will address these two problems by 1) providing quantitative means for selecting service
dogs for training and 2) providing quantifiable evidence
-
based methods for optim
al canine training techniques.


Canine training paradigms require a cognitive revolution to take advantage of recent advances in brain imaging. A
first
-
ever functional Magnetic Resonance Imaging (fMRI) study in awake, unrestrained dogs (Berns et al., 2012)

confirmed that the dog brain reward system in the caudate nucleus reacts to a primed reward hand signal. These
results provide a first
-
ever window into the brain of man’s best friend, providing a glimpse of how dogs functionally
process human trainer sign
als and to what extent different brain networks are activated by these signals.


In both the operational and clinical settings, better canine selection and screening methods would reduce training
time and costs and result in more effective service dogs. No
w, with this state
-
of
-
the
-
art canine neuroimaging tool in
hand, potential high
-
value service dogs could be screened based on their neural activation to specific handler
training cues. The hypothesis is that dogs with greater activation in the caudate nucle
us in response to handler cues
will be faster and easier to train. These experiments would result in better use of scarce canine resources (e.g., the
rare Belgian Malinois breed) and better service dogs.


The mechanisms of canine TBI and PTSD therapy effec
tiveness are not well understood, and training and
implementation methods are ripe for improvement. One hypothesis is that effective therapy dogs are better able to
sense their owner’s mental state and emotions. Some research suggests that dogs may, in fac
t, possess robust “theory
of mind” (the ability to attribute mental states such as beliefs, desires and attitudes, to another person). For example,
dogs are known to follow human’s gaze and pointing (Kirchhofer et al., 2012) and show contagious yawning, mo
re
so with their owners than with strangers (Silva et al., 2012). This method of canine neuroimaging could be used to
identify ‘brain hyper
-
social’ dogs ideally suited to TBI or PTSD therapy work. Correlating the dog's brain activity
within the caudate nuc
leus with neurophysiological markers of handler stress and anxiety could provide a screening
tool for dogs ideally suited to therapy work.


In addition to optimizing the selection of ideal service dogs, a canine neuroimaging tool could pave the way for
rev
olutionized service dog training paradigms. The identification of caudate activation by Berns et al. (2012)
demonstrates that canine
-
imaging studies could quantify the relationship between handler signal and intrinsic reward
without reliance on a behaviora
l proxy. Currently, handlers must reward approximations of a desired behavior to
teach a dog a desired task. However, associations can be made prior to behavioral manifestation. Monitoring brain
activation in real
-
time could allow trainers to reward proper

brain activation patterns indicative of associative
learning. These methods could be used to quickly measure how effective a given training technique is and provide
quantitative, evidence
-
based rationale for selecting superior training methods. They would

also increase the speed
and efficacy of canine training, useful in both operational and therapy domains.

DARPA
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Advances in understanding the influence of dog training techniques on the canine brain 1) will enhance selection of
highly
-
trainable work dogs and 2)

will enable faster, cheaper, and more effective training of military work and
therapy dogs. Overall, this project represents a radical new method of quantitatively measuring cross
-
species
communication, coordination, and therapeutics.


PHASE I: Develop a
reproducible training method for imaging canines while awake and unrestrained. Previous
work involved training only two dogs and was trial
-
and
-
error based (Berns et al., 2012). A more stream
-
lined
method will be needed for quickly and reliably training ser
vice dogs. The small business’s expertise in dog training
will be particularly crucial for this objective.


In Phase I, animal use protocols will be developed and approved, per normal procedures. Initial work in this field
has validated that animals can
be trained for safe and humane scanning in the fMRI (Berns et al, 2012). Similar
methods employed in this study will be needed in future dog imaging studies. The large size of some training dogs
presents a technical challenge for positioning in the scanner
. Equipment modifications will be completed in Phase I
to ensure proper access to the scanner and canine comfort in the experiments. Phase I deliverables will include 1) a
technical report and brief describing the training method, and 2) a set of experimen
ts demonstrating proof of concept
for scanning reward
-
related brain activity in the service dogs.


PHASE II: Finalize and validate a training method for training large dogs to undergo fMRI scanning while awake
and unrestrained. Establish performance param
eters through experiments that produce reliable brain images of
responses to trainers’ hand cues, which can be used to test ideal military dog training methods. Develop,
demonstrate, and validate protocols that combine canine imaging and simultaneous human

neurophysiological
measures in order to examine dog
-
human interactions. Apply these protocols to study what dogs are best suited for
use in therapeutic situations and quantify the relationship between this suitability and clinical outcomes. Required
Phase

II deliverables will include a technical report and brief describing the training methods and findings from
canine brain scans, as well as feasibility of use in future commercial and/or military applications.


PHASE III: Law enforcement agencies train an
d use work dogs for many of the same operations as the military;
therefore, transition to this customer would be seamless. Improved canine training techniques could also be used by
commercial dog training organizations, for behavior improvement or therapy
applications. Training techniques
developed in Phase I and II will substantially reduce canine training time and costs by selecting ideal dogs and
optimizing training techniques. These techniques will be transitioned to the US Air Force, which runs the DoD

Military Working Dog Program from Lackland AF Base, San Antonio, TX (341st Training Squadron).


Advances from this program could also be transitioned to the Veterans Administration, which is running a clinical
trial on the impact of therapy dogs on the li
ves of veterans diagnosed with PTSD. Understanding the mechanism and
communication between canine and human will facilitate therapy dog support for veterans with PTSD.


REFERENCES:

1) Berns GS, Brooks AM, Spivak M. 2012. Functional MRI in awake unrestrai
ned dogs. PLoS One.
2012;7(5):e38027. Epub 2012 May 11.


2) Kirchhofer KC, Zimmermann F, Kaminski J, Tomasello M. 2012. Dogs (Canis familiaris), but not chimpanzees
(Pan troglodytes), understand imperative pointing. PLoS One. 7(2):e30913.


3) Silva K, Bess
a J, de Sousa L. 2012. Auditory contagious yawning in domestic dogs (Canis familiaris): first
evidence for social modulation. Anim Cogn. Jul;15(4):721
-
4.


KEYWORDS: Enhanced training, improved therapy, PTSD, stress, neural correlates, brain imaging, cross
-
species
communication




ST13A
-
002


TITLE:
High
-
bandwidth, Low
-
sensitivity Optomechanical MEMS Accelerometers


DARPA
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9


TECHNOLOGY AREAS: Sensors, Electronics


OBJECTIVE: Develop a chip
-
integrated optomechanical micro
-
electromechanical systems (MEMS) acceleromet
er
with 100 ng/Hz^1/2 sensitivity and 10 kHz bandwidth using high finesse optics to readout and dynamically tune
sensor parameters.


DESCRIPTION: Inertial navigation systems (INS) are a critical asset to the DoD in environments where GPS is
either denied o
r unavailable. At the heart of these systems are precision acceleration and rotation sensors. Recently,
MEMS
-
based accelerometers have found widespread use in INS owing to their small size and ease of fabrication.
However they still lack the sensitivity an
d bandwidth required for accurate long
-
distance navigation. Typically,
MEMS accelerometers use capacitive measurement; their sensitivities are limited by thermal
-
electronic noise in the
readout circuitry [1]. Optical interferometric methods eliminate elect
ronic noise and can approach the thermal
-
mechanical limit [2], [3]. This thermal
-
mechanical noise imposes a fundamental trade
-
off between the sensitivity
(ath) and bandwidth (BW) of the accelerometer: ath proportional to (BW/mQ)^1/2, where m is the mechani
cal
resonator mass and Q is its quality factor. Therefore, to achieve a high sensitivity for a given bandwidth, the product
mQ needs to be maximized. Furthermore, for high bandwidth devices, a high resolution displacement (x)
measurement is required (x pro
portional to BW^
-
2), thus imposing requirements on the finesse (F) and input power
(P) of the optical readout cavity (x proportional to (F^
-
1P^
-
1/2)), which is ultimately limited by laser shot noise. For
example, to achieve a sensitivity of a few ng/Hz^1/2

at a bandwidth of 10 kHz, one would require mQ > 1 kg and F
> 1000. Such a sensitivity and bandwidth combination has not been achieved in a commercial device and would
reduce the INS error, allowing longer
-
duration navigation in the absence of GPS.


Recen
tly, accelerometers based on optomechanical devices have been developed, which exhibit a sensitivity of a
few ng/Hz^1/2 with a bandwidth greater than 10kHz, in a compact form
-
factor [4], [5]. Optomechanical devices are
strongly coupled optical and mechanic
al systems, in which a high finesse optical cavity is used to both measure and
manipulate high
-
quality MEMs. Such devices have enabled optical radiation
-
pressure cooling of MEMs to their
quantum ground state [6], eliminating thermal noise and enhancing the

achievable bandwidth by broadening the
mechanical resonance without loss of sensitivity. Furthermore, the cavity
-
enhanced optical field enables
displacement measurement at the standard quantum limit [7], an important fundamental limit for acceleration
sen
sing. Finally, utilizing the high circulating power achievable in a high finesse cavity, one can dynamically control
the bandwidth of the MEMS accelerometer via the optical spring effect [8], thus enabling unprecedented in
-
situ
control of accelerometer per
formance.


While optomechanical devices have demonstrated exciting results in the laboratory, significant development is
necessary to construct a robust packaged device that incorporates the laser, the optomechanical device, and optical
readout circuitry.


PHASE I: Design a robust, packaged MEMS accelerometer with high
sensitivity optical readout approaching the
standard quantum limit for displacement measurement. Such a system should exhibit high optical
mechanical
coupling such that a pump laser can man
ipulate MEMS parameters such as resonance frequency and damping rate.
The chosen work should be compatible with an accelerometer with less than100 ng/Hz^1/2 sensitivity and greater
than a 10 kHz bandwidth. Exhibit the feasibility of the approach through a
laboratory demonstration. Phase I
deliverables will include a design review including expected device performance and a report presenting the plans
for Phase II. Experimental data demonstrating feasibility of the proposed device is favorable.


PHASE II: Fa
bricate and test a prototype device demonstrating the device performance outlined in Phase I. The
Transition Readiness Level to be reached is 5: Component and/or bread
-
board validation in relevant environment.


PHASE III: Once developed, compact, integrat
ed optomechanical accelerometers with high
-
sensitivity and high
-
bandwidth would greatly improve military inertial navigation systems, requiring less frequent error correction and
updates from GPS. Innovations in Phases I and II will enable such devices to
transition out of the laboratory and into
fieldable devices. MEMS accelerometers find widespread use in civilian products such as cellphones, seismic
detection (geo
-
physical and oil exploration), automobiles and gravitational wave detection.


REFERENCES
:

DARPA
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10


1) G. Krishnan, C. Kshiragar, G. K. Ananthasuresh, and N. Bhat, “Micromachined high resolution accelerometers,”
Journal of the Indian Institute of Science, vol. 87, no. 3, Jul. 2007.


2) M. A. Perez and A. M. Shkel, “Design and Demonstration of a Bulk
Micromachined Fabry

Perot mico
-
g
-
Resolution Accelerometer,” IEEE Sensors Journal, vol. 7, no. 12, pp. 1653
-
1662, Dec. 2007.


3) K. Zandi, J. A. Bandlanger, and Y.
-
A. Peter, “Design and Demonstration of an In
-
Plane Silicon
-
on
-
Insulator
Optical MEMS Fabry P
erot
-
Based Accelerometer Integrated With Channel Waveguides,” Journal of
Microelectromechanical Systems, vol. PP, no. 99, pp. 1
-
7, 2012.


4)
R
eference
removed by TPOC on 2/19/13.


5) A. G. Krause, M. Winger, T. D. Blasius, Q. Lin, and O. Painter, “A micr
ochip optomechanical accelerometer,”
arXiv:1203.5730, Mar. 2012.


6) J. Chan, T. P. M. Alegre, A. H. Safavi
-
Naeini, J. T. Hill, A. Krause, S. Groblacher, M. Aspelmeyer, and O.
Painter, “Laser cooling of a nanomechanical oscillator into its quantum ground
state,” Nature, vol. 478, no. 7367,
pp. 89

92, Oct. 2011.


7) G. Anetsberger, E. Gavartin, O. Arcizet, Q. P. Unterreithmeier, E. M. Weig, M. L. Gorodetsky, J. P. Kotthaus,
and T. J. Kippenberg, “Measuring nanomechanical motion with an imprecision below th
e standard quantum limit,”
Phys. Rev. A, vol. 82, no. 6, p. 061804, Dec. 2010.


8) Q. Lin, J. Rosenberg, X. Jiang, K. J. Vahala, and O. Painter, “Mechanical Oscillation and Cooling Actuated by
the Optical Gradient Force,” Phys. Rev. Lett., vol. 103, no. 1
0, p. 103601, 2009.


KEYWORDS: Accelerometer, optomechanics, optics, MEMS, Fabry
-
Perot cavity, radiation pressure, optical
cooling




ST13A
-
003


TITLE:
Development of Gravitational Radiation Technology for Military Applications


TECHNOLOGY AREAS: Informati
on Systems


OBJECTIVE: Demonstrate key technologies to enable application of gravitational radiation theory and research to
military communications and navigation.


DESCRIPTION: There is a need for world
-
wide communications and navigation systems which do

not need a sky
-
view link or line
-
of
-
sight and which are less vulnerable to threat activity. Satellite communication and navigation
systems are vulnerable to interdiction and are expensive to maintain and operate.


One, very high risk approach is the ada
ptation of gravitational radiation (GR) to communications. GR is unaffected
by obstructions such as the mass of the earth and thus offers a promise of world
-
wide, ground
-
based
communications and navigation systems.


The scientific communities of the Unite
d States and other countries have devoted substantial resources to GR theory
development, technology development, and experimentation to observe cosmological radiation. The first scientific
experiments to detect GR were performed in the U.S. with weber ba
rs. More recently, the U.S. has expended
significant resources in developing the science and technologies for the Laser Interferometer Gravitational
-
Wave
Observatory (LIGO). Foreign countries are also investing in research in similar activities such as M
iniGRAIL (in
The Netherlands), Virgo (in Italy), GEO 600 (in Germany), and TAMA 300 (in Japan). The scientific community is
optimistic that GR will be directly detected within the next decade.


The transition of the GR science and technologies to militar
y GR applications requires significant additional
innovative research in several enabling technology areas beyond those of interest to the cosmological GR
DARPA
-

11


researchers. A successful GR communications system will require both a GR transmitter and a GR recei
ver.
Current technology development is focused solely on GR detectors. The system needs to allow adequate bandwidth
for communications. Current scientific GR detectors operate in the sub
-
Hz to few KHz range. The size of the GR
system needs to be milita
rily useful. The current LIGO systems in Washington and Louisiana have detector arms
several kilometers long. Implicit in the above is the most significant challenge, i.e., the detection of gravitational
radiation. GR has not yet been directly detected.


This topic seeks innovative concepts for the application of GR to military communications. The concept should be
supported by scientific literature or analysis based upon general relativity theory or quantum mechanics theory. The
concept should provide

sufficient detail to permit the high
-
level visualization of a system and the identification of
key technologies that need to be developed. A field or laboratory validation of one or more key technologies is
essential. The maturation of the concept shoul
d be phased with definitive advancements in technology.


PHASE I: Develop the underlying scientific approach to achieving a GR
-
based military communications system.
Define the underlying technologies required to implement the system. Perform an analysis
of the proposed system
to include an estimate of the magnitude of GR emitted and an estimate of the sensitivity of the GR receiver.


PHASE II: Conduct an experiment to demonstrate one or more of the critical technologies needed to implement a
system. The

focus should be on the generation and detection of a GR carrier wave and not on the transmission of
information. A fully successful experiment would result in the generation and detection of GR.


PHASE III: Initially, a successful GR communications sy
stem could replace existing high
-
priority communications
with ground
-
based systems to reduce vulnerability. Eventually, it could replace satellite
-
based communications and
navigations systems. Eventually a successful GR communications system would replace

existing high capacity,
long
-
haul point
-
to
-
point communications systems. This would reduce requirements for extensive ground
infrastructure and maintenance.


REFERENCES:

1) Stephen J. Minter, Kirk Wegter
-
McNelly, Raymond, Y. Chiao, "Do Mirrors for Gra
vitational Waves Exist?"
arXiv.org, "http://arxiv.org/abs/0903.0661".


2) Robert M. L. Baker, Jr., "The Li
-
Baked High Frequency Relic Gravitational Wave Detector," 12 August 2010,
"http://gravwave.com/docs/2010 Russia Lect .ppt".


3) R. Clive Woods, Robe
rt M.L. Baker, Fangyu Li, Gary V. Stephenson, Eric W. Davis, Andrew W. Beckwith, "A
New Theoretical Technique for the Measurement of High
-
Frequency Relic Gravitational Waves," Journal of
Modern Physics, 2011, 2,498
-
518, "http://www.scirp.org/journal/PaperI
nformation.aspx?paperID=5625"


4) L. Gottardi, A. de Waard, A. Usenko, and G. Frossati, "Sensitivity of the spherical gravitational wave detector
MiniGRAIL operating at 5 K.", 1 May 2007, "http://arxiv.org/pdf/0705.0122v1.pdf"


5) Website: High Frequency

Gravitational
-
Wave Detector,
"http://www.sr.bham.ac.uk/gravity/project.php?project=MHzDetector".


KEYWORDS: gravitational radiation, gravitational waves, general relativity, quantum mechanics




ST13A
-
004


TITLE:
A Flexible and Extensible Solution to Inco
rporating New RF Devices and

Capabilities
i
nto EW/ ISR Networks


TECHNOLOGY AREAS: Information Systems


OBJECTIVE: Develop a solution that will allow for seamless insertion of new Radio Frequency (RF) devices and
capabilities into EW/ISR networks. The newl
y added devices/capabilities should be readily available for providing
DARPA
-

12


services to the various applications running on the network. The goal is to support addition of new devices to
multifunction networks in the field, without software changes elsewhere in

the network.


DESCRIPTION: In military applications, RF devices constitute a heterogeneous network of receivers/ transmitters
deployed primarily for the purpose of communicating tactical information. However, current RF devices are highly
versatile and th
us have the potential of fulfilling various functions in support of various tasks such as Situational
Awareness, Electronic Warfare/Intelligence, Surveillance and Reconnaissance (EW/ISR). In the highly dynamic
warfare environment, such EW/ISR networks shou
ld be easily extendable to incorporate new device types and to
support additional applications [1].


One of the prerequisites for achieving this goal is the development of a language that can be used to describe both
the capabilities of RF components and t
heir current operational status. While some limited capabilities of this kind
could be achieved by the use of XML coupled with an appropriate DTD [2], such an approach would be limited by
the XML’s lack of formal semantics. In particular, descriptions of d
evice capabilities would have to be provided in a
strictly prescribed format in order to be processed by the network infrastructure. Exchange of capability descriptions
would consume substantial bandwidth, since complete descriptions would need to be sent.

And finally, any
extension of the device types or status information would require a modification of the software that interprets XML
descriptions.


To avoid the above
-
described problems, this topic seeks development and/or specialization of a representat
ion with
formal, computer
-
processable semantics. It is highly desirable that the representation be based on a standard
language. Examples of such semantic languages are Web Ontology Language (OWL) [3] and Rule Interchange
Format (RIF) [4]. Prior work in th
is area has resulted in an ontology to describe the various aspects of the RF device
structure and functionality [5]. However, this ontology is not sufficient for describing all of the characteristics of RF
devices and their operational status needed for a
n EW/ISR network. Moreover, this work has not been demonstrated
in relevant scenarios. The development of such an ontology is a complex task since it requires not only coverage of
the relevant concepts of the domain, including complex relationships among t
he concepts, but also representing the
concepts and the structures of knowledge in a form that a wide and diverse community of RF experts can agree on.


Furthermore, this topic seeks innovative research on automated tools that can automatically incorporate

new devices
into an RF Situation Awareness or EW/ISR network. The research should result in a solution that demonstrates
seamless incorporation and use of the descriptions of RF components and their status by the network infrastructure.


PHASE I: Develop
an ontology appropriate for describing typical RF devices and device status information, relevant
for use of those devices to support EW/ISR tasks. Select a standards
-
based representation language and propose any
extensions to the language that are necessa
ry to effectively represent the ontology. Assess the limits of
expressiveness of the ontology and of the language (as extended) with respect to both current and future RF devices
and device status. Develop scenarios for testing the use of the ontology and
language in a command and control
system that selects an RF device to carry out a specified reception, transmission and/or processing task. Demonstrate
the developed solution in a simulated environment. Interact with organizations and programs that may be
users of
the technology to assess requirements and improve their understanding of its benefits.


PHASE II: Evolve the ontology and extend the language as needed. Design and implement a run time prototype
system that supports use of the descriptions of RF c
omponents and their status in a command and control system that
selects an RF device to carry out specified reception, transmission and/or processing tasks. Develop a test
environment for evaluating the run time system under the scenarios developed in Phas
e I. Carry out evaluation
experiments accordingly. Interact with organizations and programs that may be users of the technology and adjust
the ontology, language, run time system design, implementation strategy, scenarios and tests to maximize
probability
of successful adoption.


PHASE III DUAL USE APPLICATIONS: There is a critical military need for RF situational awareness and other
EW/ISR capabilities that exploit large numbers of networked sensors and transmitters. Work is ongoing on methods
to exploit R
F devices already in the field for other purposes to support such capabilities [1], reducing or eliminating
the cost of deploying special
-
purpose devices. Products based on the technology developed in this project will more
readily extend to incorporate a
larger range of devices, thus facilitating more rapid deployment and wider
availability of the new EW/ISR network capabilities such as RF situational awareness. Similarly, benefits are
DARPA
-

13


expected in command and control systems for commercial RF device networ
ks. One expected application is real
-
time reallocation of spectrum among multiple cellular and public safety wireless networks enabling increased civil
data communications in normal conditions and increased public safety communications in emergency situati
ons
without increasing total spectrum requirements. Achieving this benefit requires broad
-
area real
-
time RF situational
awareness, which will be made more affordable and more precise through flexible addition of heterogeneous devices
to the sensor network
as enabled by the results of this project.


REFERENCES:

1) Advanced RF Mapping (RadioMap) Program. Solicitation Number: DARPA
-
BAA
-
12
-
26. Defense Advanced
Research Projects Agency, March 27, 2012.


2) Extensible Markup Language (XML) 1.0 (Fifth Edition). W3
C Recommendation, 26 November 2008.


3) OWL Web Ontology Language

Overview. W3C Recommendation, 10 February 2004.


4) RIF Overview. W3C Working Group Note, 22 June 2010.


5) Wireless Innovation Forum “Description of the Cognitive Radio Ontology”, Technical

Report

WINNF
-
10
-
S
-
0007, September 30 2010. Available at http://groups.winnforum.org/d/do/ 3370.


KEYWORDS: RF devices, device capabilities, capability descriptions, ontology for RF devices.




ST13A
-
005


TITLE:
Modeling and Optimizing Turbines for Unstea
dy Flow


TECHNOLOGY AREAS: Air Platform, Ground/Sea Vehicles


OBJECTIVE: Develop an analytical software tool capable of modeling and optimizing turbine components for
unsteady flow conditions.


DESCRIPTION: Conventional gas turbine engines rely on Cons
tant Pressure Combustion (CPC) to generate the
enthalpy needed to provide the horsepower and thrust that our warfighters need. Unfortunately, CPC is a very
inefficient process and approximately 30
-
40% of the energy contained in a unit of fuel is wasted.
The ability to
create greater efficiency and power density using current gas turbine technology and design is extremely limited and
the marginal rate of return in dollars and technology invested versus efficiency and power density is decreasing.
The DoD a
nd Industry spends millions of dollars to achieve fractions of a percent increase in fuel efficiency.
Increased SFC directly translates into greater range, endurance and capability for our military.


Pressure Gain Combustion (PGC) addresses the largest so
urce of inefficiency in gas turbine engines and offers the
greatest potential for improving combustion efficiency and reducing Specific Fuel Consumption (SFC). It is
estimated that integrating this technology into current or future engines will decrease S
FC by 10
-
20% and increase
power density by 20%. Although PGC has demonstrated efficiency, it is not without its drawbacks. Almost every
PGC concept developed whether Pulse Detonation Engines (PDE), Rotating Detonation Engines (RDE) or Wave
Rotor introduc
es unsteady flow conditions. Conventional gas turbines are optimized for steady flow conditions and
introduction of unsteadiness in pressure, temperature, and/or swirl angle can have detrimental effects on turbine
efficiency. Without the development of a h
ighly efficient turbine capable of operating across a wide range of
temperatures, pressures, and incidence angles, all gains made by the combustors will be lost when PGCs are
integrated with turbines. Efficient turbines capable of operating in highly unste
ady regimes are needed in order to
fully achieve the energy benefits PGCs offer. The current State of the Art for this technology is TRL 2. At the end
of this STTR it is anticipated that an optimized turbine can be designed and tested to validate the sof
tware.


PHASE I: Develop an analytical software tool capable of modeling and optimizing turbine components in unsteady
flow. Select current or previous PGC data (unsteady flow to the turbine) as input to develop an analytical software
tool capable of mo
deling and optimizing turbine components for unsteady flow conditions and increasing efficiency.
The Phase I deliverables will include monthly status reports and a Final report.

DARPA
-

14



PHASE II: Utilize the software tool developed in Phase I to design and manu
facture an optimized first stage high
pressure turbine and test it in an operationally relevant environment. The target Technology Readiness Level (TRL)
for this component should be 4
-
5. Deliverables include: a prototype of the optimized high pressure turb
ine, monthly
status reports, and a final report that contains test data from the optimized component.


PHASE III: This technology is applicable to the Navy, Air Force, Army, and Marine Corps gas turbine engines and
their use in aircraft, ground vehicle, an
d ship propulsion. Significant fuel cost savings, reduced logistics footprint,
and an overall increase in turbine efficiencies will reduce dependency on fuel and have a profound impact on
national security. This technology has commercial gas turbine appl
ication in aircraft and commercial ship
propulsion; and gas turbine
-

power generation. The ability to model and optimize turbine components for unsteady
flow conditions is essential in the ability to design pressure gain combustion turbine engines in the

future. Pressure
gain combustion technology has the potential to reduce specific fuel consumption by 20% and increase power
density by 20%.


REFERENCES:

1) Mattingly,
J. D., “Elements of Gas Turbine Propulsion”, McGraw
-
Hill, 1996.


KEYWORDS: Turbines,

Pressure Gain Combustion, Pulse Detonation, Rotating Detonation, Wave Rotor




ST13A
-
006


TITLE:
Novel Extensible Design Approaches for Advanced Aircraft Composite

Structural Architectures


TECHNOLOGY AREAS: Air Platform, Materials/Processes


OBJECTIVE: D
efine a low
-
level
,

stochastically verified
,

composite structural toolset geared towards expediting
aircraft design and development, while at the same time leveraging

a

building
-
block approach to structural
verification for enhanced airframe assurance.


DE
SCRIPTION: Advanced composites
enable high performance aerospace structures, including extensive tailoring
to particular applications, fastener elimination, weight reduction, improvements in fatigue resistance, and corrosion
prevention. Some essential chal
lenges for modern composite design, fabrication, and certification include the
integration of structural design detail with repeatable manufacturing processes, which must include both material
and process control. Typically, the design problem is dominated

by considerations of design details, manufacturing
flaws, and service damage, all of which cause local stress concentrations.


Robust approaches to structural assurance explore strength, fatigue, and damage tolerance issues, and tend to have a
high depen
dency on multi
scale sample tests. This design and testing approach tends to have enormous cost and
schedule impacts, effectively raising the barrier to entry of advanced composite structures into major DoD
platforms.


This effort intends to develop struct
ural architectures that speed development and qualification of composite aircraft,
which has broad benefits to DoD, DARPA, and the private sector in reducing cost, increasing content re
-
use, and
improving time
-
to
-
market.


In particular, novel solutions are

sought that would allow extensive re
use of parametric elements in structural design
of composites to achieve expedited design, verification, validation, and airworthiness certification or qualification.
By raising the level of structural design abstracti
on to higher orders, both design engineering and verification
activities could be effectively abbreviated while increasing design confidence.


While conventional design processes use a set of material allowables verified at c
oupon
level, the end goal of th
is
effort would be to develop a stochastically validated, open, extensible database typical aircraft component
geometries, which include allowable properties, based on key parameters for geometry, materials, and defined
manufacturing process standards.

DARPA
-

15



These properties should be applicable to a defined set of configurations for key primary and secondary structural
elements, including for example, spars, ribs, skins, doors, landing gear, and associated composite to composite and
composite to metal joints
. Each of these components should include definition of parameters that permit sizing to
necessary loads, and consideration of buckling and other potential failure modes of the structures based on probable
load applications.


For reference and guidance, on
e may refer to the government publication, ANC
18, which defines properties for
wooden aircraft structural materials and guidelines for structural member and joint design. Although obsolete,
publication ANC
-
18 offers relevant guidance to this effort, beca
use it provides a novel
set

of design rules for non
-
homogenous structures. Wood, considered the original filamental composite, is actually a more complex material to
design with, possessing more key parameters on type, condition, and alignment of the mater
ial with loads than are
normally considered for modern composites in airframes.


PHASE I: Design and specify a preferred material set and set of basic components, perform analytic justification of
chosen parametric geometries. Define robust approach for u
ncertainty characterization and tracking. Develop an
analysis of predicted performance, and define key technological milestones. Phase I deliverables will include a
description of the proposed material set, proposed component set, analytic justification of

broad aerospace
applicability, and definition of processes required to quantify and track performance uncertainty from design
through certification.


PHASE II: Develop, demonstrate, and validate the basic approach to component parametric definition, stoch
astic
verification, and quantification and tracking of uncertainties. It is anticipated that this demonstration will occur in a
laboratory setting, but demonstrate multi
scale parametric element application, uncertainty quantification, stochastic
verificat
ion, design application, process verification, and representative simulation in a certification process flow.


PHASE III: This novel architectural approach
has potential for use in civil
-
certified aircraft structures, inclusive of
aircraft certified to 14
CFR PART 23 and 14 CFR PART 25. If successful, this methodology has the potential to
directly transition to the Air Force Research Laboratory’s Composites Affordability Initiative. Additionally, future
unmanned aircraft programs, including demonstration p
rograms executed by DARPA, may have particular benefit
from this structural architecture approach and associated methodology. An alternate military transition path would
be inclusion of this structural approach into a future aircraft program of a record.


REFERENCES:

1) MIL
HDBK
17, Composite Materials Handbook


2) ANC
18

Design of Wood Aircraft Structures, Code of Federal Regulations (CFR), Title 14 (Aeronautics and
Space), 14

CFR Part 23, and 14 CFR Part 25, FAA Advisory Circular AC 20
-
107B “Composit
e Aircraft Structure”


3)

Code of Federal Regulations (CFR), Title 14 (Aeronautics and Space), 14 CFR Part 23, and 14 CFR Part 25,


4)

FAA Advisory Circular AC 20
-
107B “Composite Aircraft Structure”


KEYWORDS: Composites; Design; Paramtric; Certificatio
n